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TO GO DIRECTLY TO THE TECHNICAL ORDER, CLICK ON THE CONTINUE BUTTON.
WELCOME TO TECHNICAL ORDER 00-105E-9, 1 FEBRUARY 2006, REVISION 11.
TO SEE THE SEGMENT INFORMATION CHANGE NOTICE, CLICK ON THE NOTICE BUTTON.
TO CONTACT THE TECHNICAL CONTENT MANAGER , CLICK ON THE CONTACT BUTTON.
CONTINUE
NOTICE
CONTACT
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CLICK ON THEBOOKMARKS ANDCLICK ON THE (+)SYMBOLS, THEN
CLICK ON SUBJECTLINKS TO GO TOSPECIFIC VIEWS
IN THIS SEGMENT.
THIS IS SEGMENT 20 COVERING CHAPTER 18 FROM THE 707 TO THE 737.
TECHNICAL ORDER 00-105E-9 TECHNICAL CONTENT MANAGER
WRITTEN CORRESPONDENCE:
HQ AFCESA/CEXFATTN: Fire and Emergency Services Egress Manager139 Barnes Drive Suite 1Tyndall AFB, Florida 32403-5319
E-MAIL: HQAFCESA.CEXF@tyndall.af.mil
INTERNET: HQ AFCESA Fire and Emergency Services PUBLIC WEB PAGE: http://www.afcesa.af.mil/CEX/cexf/index.asp Safety Supplements: http://www.afcesa.af.mil/CEX/cexf/_firemgt.asp
PHONE: (850) 283-6150DSN 523-6150
FAX: (850) 283-6383DSN 523-6383
For technical order improvements, correcting procedures, and other inquiries,please use the above media most convenient.
This page is provided to notifiy the user of any informational changes made to Technical Order 00-105E-9 in this Segment and the currentRevision. Informational changes will be referenced in the Adobe Reader’s Bookmark tool as a designator symbol illustrated as a <[C]> forquick reference to the right of the affected aircraft. The user shall insure the most current information contained in this TO is used for hisoperation. Retaining out of date rescue information can negatively affect the user’s operability and outcome of emergencies. If the user printsout pages his unit requires, the user shall print the affected page(s), remove and destroy the existing page(s), and insert the newly printedpage(s) in the binder provided for that purpose. A Master of this TO shall be retained in the unit’s library for reference, future printingrequirements and inspections.
CHAPTER AIRCRAFT PAGE EXPLANATION OF CHANGE
SEGMENT 20 INFORMATION CHANGE NOTICE
None.
TO 00-105E-9
Chapter 18 Cover
NOTE
Chapter 18 contains emergency rescue andmishap response information for the following aircraft:
DC-3DC-6DC-7DC-8DC-9
DC-10MD-11MD-80MD-90
L-1011-1L-1011-500
707717720727737747757767777
707T.O
. 00-105E-9
707. AIRCRAFT PAINT SCHEME1
707T.O
. 00-105E-9
707. AIRCRAFT DIMENSIONS
Height 42’ 1” (12.83 M)
Length 152’ 11” (44.42 M)
Wing Span 145’ 9” (45.42 M)
707-320B/C
707-120B 707-320/-420
Wing Span 142’ 5” (44.42 M) Wing Span 130’ 10” (39.83 M)
Length 138’ 10” (42.32 M)
Height 41’ 8” (12.70M) Height 42’ 2” (12.85M)
Length 145’ 6” (44.35 M)
2
707T.O
. 00-105E-9
707.3 AIRCRAFT SKIN PENETRATION POINTS
AFT CARGO DOOR CENTER CARGO DOOR FWD CARGO DOOR
8”
2”
HANDLE
PENETRATIONPOINT
PENETRATIONPOINT
PENETRATIONPOINT
HANDLE
HANDLE
10”
3”
2”
2”
FWDFWDFWD
707T.O
. 00-105E-9
707.4 AIRCRAFT SKIN PENETRATION POINTS-Continued707-120B-320C TURBOFAN ENGINES
707-120B-320C TURBOFAN ENGINES
LEFT SIDE OF ENGINE
RIGHT SIDE OF ENGINE
COMMON POINT (LH & RH SIDE)
RIGHT SIDE OF ENGINE
LEFT SIDE OF ENGINE
COMMON POINT (LH & RH SIDE)
FORWARDENGINE MOUNT
213.942 AFTENGINE MOUNT MID SPAR
STRUT
COWLSPLIT COWL SPLIT
ENGINE
OUTBOARD NACELLE AND STRUT LEFT SIDE VIEW
OUTBOARD NACELLE AND STRUT LEFT SIDE VIEW
ENGINE
MID SPAR
COWL SPLIT
COWLSPLIT
STRUT
213.942 AFTENGINE MOUNT
136.00 FORWARD ENGINE MOUNT
T/C FAIRING
FIRESEAL
FIRESEAL
707T.O
. 00-105E-9
707.5
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw24 Foot Ladder35 Foot LadderFire Drill IIAIRCRAFT ENTRY-100/-200 SERIES
1. NORMAL/EMERGENCY ENTRY
a. Overwing escape hatches both sides- Push red panel, located top center of hatches, in and push hatches inward.
b. Pull handle, located left side forward and aft entry doors, outward and rotate clockwise.
c. Pull handle, located forward and aft galley doors right side, outward and rotate counter- clockwise.
d. Press red handle, located on escape hatch top right forward crew compartment, and pull out.
2. CUT-IN
a. Cut along window lines as last resort.
NOTE: Some series are equipped with class one escape hatches.
CAUTION
For passenger and service doors, emergency slide will automatically deploy when doors are opened externally.
NOTE: Refer to the C-135 for more extensive information. Both airframes are identical except cargo and tanker capabilities.
434 GALS(1643 LITERS)
2333 GALS(8831 LITERS)
2283 GALS (8642 LITERS)
434 GALS(1643 LITERS)
2333 GALS(8831LITERS)
2283 GALS(8642 LITERS)
UTILITY & AUXILIARY RESERVOIRIN AFT CARGO COMPARTMENT
PASSENGER OXYGENSYSTEM BOTTLES IN AFTCARGO COMPARTMENT
PORTABLE OXYGENBOTTLES OR NEARFLOOR LEVEL ONPARTITIONS
HYDRAULICACCUMULATORS(RIGHT WHEELWELL AREA)
FIRE EXTINGUISHERPORTS ON ENGINERIGHT COWLING(TYPICAL EACH ENGINE)
CREW OXYGEN SYSTEMBOTTLES IN FWD LOWEREDCEILING OR FWD CARGO AREA
7306 GALS(27,656 LITERS)
ENGINE OIL TANK-EACHENGINE-RIGHT SIDEPORTABLE OXYGEN BOTTLE ON
FORWARD SIDE OF BULKHEAD
BATTERIES
28” 28”38”
1cGALLEY DOOREXTERNAL HANDLE
1aPANEL
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
NOTE: 2 inch band of contrasting color around all doors, windows and hatches operable from outside the aircraft.
GALLEY DOOR(RT SIDE ONLY)
ON CARGOACFT ONLY
AFT ENTRY DOOR
CUT-IN AREA EACH SIDE OF ACFT (NOT MARKED ON ALL ACFT)
EMERGENCY EXITS
FWD ENTRYDOOR
GALLEY DOOR(RIGHT SIDE ONLY)
1bENTRY DOOREXTERNAL HANDLE
707T.O
. 00-105E-9
707.6 ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN
a. Retard thrust levers, located on pilot’s center console, to RETARD position.
b. Place engine start levers, located on pilot’s center console, to CUT OFF position
c. Pull emergency fire T-handles, located top center above instrument panel.
d. Place engine start switches, located on pilot’s overhead panel, to OFF position.
e. In case of APU fire, pull APU fire switch, located on the upper left flight engineer’s panel, out to apply agent to APU.
f. If no APU fire, place APU master switch, located on the upper left flight engineer’s panel, to OFF position.
g. Place battery switch, located on lower right flight engineer’s panel, down to OFF position.
2. AIRCREW EXTRACTION
a. Unlatch lap belts and remove shoulder harness from crewmembers.
b. Depress seat control handles, located on flight engineer’s seat, and rotate from left to right.
NOTE: If seat tracks are not damaged during crash landing, use adjustable seat controls to retract seats to aft position.
NOTE: Passenger seats are equipped with lap belts only.
APPLICABILITY: 707-100/-200 -300/-400
1cFIRE T-HANDLE
1dENGINE START SWITCHES
1gBATTERYSWITCH
1eAPU FIRE SWITCH
1fAPU MASTERSWITCH1b
START LEVERS
1aFIRE T-HANDLE
NOTE: Optional location for T-handles is on the pilot’s light shield.
707T.O
. 00-105E-9
707.7 EMERGENCY RESCUE ACCESS-100 AND -200 SERIES
CHOP OUT AREAS (NOTMARKED ON ALL AIRCRAFT)
CHOP OUT AREAS (NOTMARKED ON ALL AIRCRAFT)
AFT ENTRY DOOR
OVERWING ESCAPEHATCHES
FWD GALLEY DOOR
FWD ENTRY DOOR
FLIGHT DECK WINDOWSOPEN INTERNALLY
6 FEET 1/2 INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED
9 FEET 7INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED
AFTGALLEYDOOR
707T.O
. 00-105E-9
707.8
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw24 Foot Ladder35 Foot LadderFire Drill IIAIRCRAFT ENTRY-300/-400 SERIES
1. NORMAL/EMERGENCY ENTRY
a. Overwing escape hatches both sides- Push red panel, located top center of hatches, in and push hatches inward.
b. Pull handle, located left side forward and aft entry doors, outward and rotate clockwise.
c. Pull handle, located forward and aft galley doors right side, outward and rotate counter- clockwise.
d. Press red handle, located on escape hatch top right forward crew compartment, and pull out.
2. CUT-IN
a. Cut along window lines as last resort.
NOTE: Some series are equipped with class one escape hatches.
CAUTION
For passenger and service doors, emergency slide will automatically deploy when doors are opened externally.
NOTE: Refer to the C-135 for more extensive information. Both airframes are identical except cargo and tanker capabilities.
434 GALS(1643 LITERS)
2285 GALS(8650 LITERS)
4036 GALS (15,278 LITERS)
434 GALS(1643 LITERS)
2285 GALS(8650 LITERS)
4036 GALS(15,278 LITERS)
UTILITY & AUXILIARY RESERVOIR(LEFT FILLET AREA)
PASSENGER OXYGENSYSTEM BOTTLES IN AFTCARGO COMPARTMENT
PORTABLE OXYGENBOTTLES 8 PLACESON HATRACKS ORNEAR FLOOR LEVELON PARTITIONS
HYDRAULICACCUMULATORS(RIGHT WHEELWELL AREA)
FIRE EXTINGUISHERPORTS ON ENGINERIGHT COWLING(TYPICAL EACH ENGINE)
CREW OXYGEN SYSTEMBOTTLES IN FWD LOWEREDCEILING OR FWD CARGO AREA
10,190 GALS(38,573 LITERS)
ENGINE OIL TANK-EACH ENGINE-RIGHT SIDE
PORTABLE OXYGEN BOTTLE ONFORWARD SIDE OF BULKHEAD
BATTERIES
28” 28”38”1cGALLEY DOOREXTERNAL HANDLE
1aPANEL
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
NOTE: 2 inch band of contrasting color around all doors, windows and hatches operable from outside the aircraft.
GALLEY DOOR(RT SIDE ONLY)
ON CARGOACFT ONLY
AFT ENTRY DOOR
CUT-IN AREA EACH SIDE OF ACFT (NOT MARKED ON ALL ACFT)
EMERGENCY EXITS
FWD ENTRYDOOR
GALLEY DOOR(RIGHT SIDE ONLY)
1bENTRY DOOREXTERNAL HANDLE
APU FUELLINE
APU FWD CARGOCOMPARTMENT ON25000 SERIES
707T.O
. 00-105E-9
707.9 EMERGENCY RESCUE ACCESS-300 AND -400 SERIES
CHOP OUT AREAS (NOTMARKED ON ALL AIRCRAFT)
CHOP OUT AREAS (NOTMARKED ON ALL AIRCRAFT)
AFT ENTRY DOOR
AFTGALLEYDOOR
OVERWING ESCAPE HATCHES
FWD GALLEY DOOR
FWD ENTRYDOOR
FLIGHT DECK WINDOWSOPEN INTERNALLY
6 FEET 1/2 INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED
10 FEET 1INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED
CARGOAIRCRAFTONLY
707T.O
. 00-105E-9
707. CABIN CONFIGURATION-707-120B (PASSENGER)
10
137 PASSENGERS - MIXED CLASS (DOMESTIC)
142 PASSENGERS - MIXED CLASS (INTERNATIONAL)
ALL TOURIST ARRANGEMENT
GALLEY SERVICE DOOR 24X48” (61X121.9 CM)
GALLEY SERVICE DOOR 24X48” (61X121.9 CM)
MAIN ENTRY DOOR34X72” (86.4X183 CM)
MAIN ENTRY DOOR34X72” (86.4X183 CM)
32 PASSENGERS4 A BREAST AT 38”(96.4 CM) PITCH
105PASSENGERS6 A BREAST AT 34”(86.4 CM) PITCH
TYPE III EMERGENCY EXIT(LH & RH) 20X38” (51X96.5 CM)
20 PASSENGERS4 A BREAST AT 40”(101.6 CM) PITCH
122PASSENGERS6 A BREAST AT 34”(86.4 CM) PITCH
174PASSENGERS6 A BREAST AT 34”(86.4 CM) PITCH
C CLOSET
G GALLEY
L LAVATORY
S DOUBLE ATTENDANT’S SEAT C
L L G
SC C
CGG LLS
LL
G G
CS
L
L
G G C
S
L L G G
CS
L LG
S
G
C
707T.O
. 00-105E-9
707. CABIN CONFIGURATION-Continued-707-320/-320B/-420 (PASSENGER)
11
C CLOSET
G GALLEY
L LAVATORY
S DOUBLE ATTENDANT’S SEAT
ALL TOURIST ARRANGEMENT
189 PASSENGERS - 34” SEAT PITCH (86.4 CM)
141 PASSENGERS - MIXED CLASS (INTERNATIONAL)
MAIN ENTRY DOOR34X72” (86.4X183 CM)
MAIN ENTRY DOOR34X72” (86.4X183 CM)
18 FIRST CLASS 123 TOURIST
GALLEY SERVICE DOOR 24X48” (61X121.9 CM)
GALLEY SERVICE DOOR 24X48” (61X121.9 CM)
TYPE III EMERGENCY EXIT(LH & RH) 20X38” (51X96.5 CM)
GGL L
S
GL L
S
GG L L
SC L
G L L
S C L
707T.O
. 00-105E-9
707. CABIN CONFIGURATION-Continued-707-320C (CARGO/PASSENGER)
12
C CLOSET
G GALLEY
L LAVATORY
S DOUBLE ATTENDANT’S SEAT
ALL TOURIST - 194 PASSENGERS - 32.8” (82.5 CM) SEAT PITCH
7 PALLETS - 88X108” (274 CM) 69 PASSENGERS 34” (86.4 CM) SEAT PITCH
13 PALLETS - 88X125” (223X318 CM)
NOT INSTALLED ON -320C FREIGHTER
CARGO DOOR
CARGO DOOR
CARGO DOOR
THREE TO 10 PALLETS CAN BE ACCOMMODATED IN MIXED CARGO/PASSENGER CONFIGURATIONS.
TYPE III EMERGENCY EXIT(LH & RH) 20X38” (51X96.5 CM)
TYPE III EMERGENCY EXIT(LH & RH) 20X38” (51X96.5 CM)
91X134”(231X340 CM)
G G L L
SC L
GL
S
L
GL
S
GG L LS L
LL
GL
S
PASSENGERS PALLETS187 0131 3115 4103 5 87 6 69 7 57 8 33 9 29 10 0 13
717. 717T.O
. 00-105E-9
AIRCRAFT PAINT SCHEME1
717. 717T.O
. 00-105E-9
AIRCRAFT DIMENSIONS2
717-200
124’ 0”(37.8M)
77’ 11”(23.7M)
11’ 0”(3.4M) 10’ 10”
(3.3M) 52’ 8”(16.1M)
78’ 5”(23.8M)
7’ 7”(2.3M) 57’ 9”
(17.6M) 112’ 8”(34.3M)
36’ 10”(11.2M)
6’ 4”(1.9M)
16’ 0”(4.9M) 93’ 4”(28.4M)
FEET
METERS
0 10 20 30
0 5 10
717. 717T.O
. 00-105E-9
3 SKIN PENETRATION POINTSAND GENERAL INFORMATION
NOTE: The Boeing 717 is the previously named MD-95 after the design was acquired in 1997. It is the reconfigured DC-9-30.
GENERAL INFORMATION FOR ALL 717 MODELS AND VARIANTS
1. Current version is the 717-200. Available in basic and grossweight versions.
2. A proposed version is the 717-100 with 86 seats, formerly theMD-95-20.
3. Another proposed version will be the 717-100X Lite with 75seats.
4. Another proposed version will be the 717-300 for 130 seats.
SKIN PENETRATION POINTS
Fuselage (both sides)Penetrate approximately 4 inches below cabin
windows. Avoid penetrating emergency exits.
BASIC WEIGHT FUSELAGE VARIANT
ENGINE NACELLES (BOTH SIDES)PENETRATE MID-SECTION OF ENGINEBELOW ENGINE CENTERLINE
GROSS WEIGHT FUSELAGE VARIANT
717. 717T.O
. 00-105E-9
4 ENGINE DANGER AREASJET INTAKE AND BLAST DISTANCES
NOTE:· These contours are to be used as guidelines only since the operational environment varies greatly - operational varies greatly-operated safety aspects are the responsi bility of the user/planner.
· All velocity values are statute miles per hour.
· Cross winds will have considerable effect on contours.
· Sea level static-standard day-zero ramp gradient.
AFT LIMIT OF ZONE A B C
(STATUTEWIND VELOCITY MPH) 300 100 60
TAKEOFF FEET 31 178 375 POWER METERS 11 54 114
BREAKAWAY FEET NA 35 78POWER METERS NA 11 24
FEET NA 30 50IDLE POWER METERS NA 9 15
GROUND PLANE
717. 717T.O
. 00-105E-9
5 AIRCRAFT DANGER AREAS1. EXTERIOR TAILCONE JETTISON
Jettisoning tailcone allows emergency ingress or egress. Prior to selecting jettison of tailcone, insure all personnel and equipment are clear of jettison area. Failure to clear area can cause damage to equipment and death or injury to personnel.
a. Using a ladder, proceed aft of left engine, locate jettison handle access door which is 10 feet (3 meters) above ground.
b. Push door and pull control handle. Inside lock cable must be re-installed if handle is pulled.
2. INTERIOR TAILCONE JETTISON
a. Proceed aft to rear cabin bulkhead, locate jettison handle on aircraft left wall and pull control handle.
TAILCONEJETTISON AREA
JETTISONED TAILCONE
1aEXTERIORTAILCONECONTROLS
WARNING
1aTAILCONEACCESS DOOR
2aINTERIORTAILCONECONTROLS
10 FT
717. 717T.O
. 00-105E-9
6
AIRCRAFT DANGER AREAS-ContinuedAPU ACCESS DOORS AND APU EXTERIOR CONTROLS
Use extreme caution when opening access areas where fire is evident.
1. APU ACCESS DOORS
a. Insert screw driver or similar tool into slot of cam-lock fasteners.
b. Turn fasteners to the left to open.
c. Pull down access doors.
2. APU EXTERIOR CONTROLS
a. Shut off APU by pressing the APU SHUT OFF/NORMAL switch UP.
b. If FIRE warning light is illuminated indicating APUfire, flip toggle switch cover up, select FIRE AGENT1 switch and press UP to discharge fire agent.
c. If FIRE light remains illuminated, repeat step a byselecting FIRE AGENT 2 switch. FIRE light will goout if fire is extinguished.
d. If fire is not extinguished, access APU through airintake, skin penetration, or other means available.
WARNING
APU AIR INTAKE 1aAPU ACCESS DOOR
APU FIREWARNING HORN
APU EXTERIOR CONTROLS
FIRE
APU FIRE
717. 717T.O
. 00-105E-9
AIRFRAME MATERIALSNOTE: All metal wing spars, glassfibre trailing edges on wings, ailerons, flaps, elevators, rudder, and detachable wing tips. Most of cabin floor made of balsa or Nomex core sandwich.
RADOME
COMPOSITES
ENTRANCE STAIR DOOR
WING TO BODY FAIRING
FLAP HINGE FAIRINGS
TAILCONE
ELEVATOR TABSTIP CAP
HORIZONTALSTABILIZERFAIRING
7
717. 717T.O
. 00-105E-9
8
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw35 Foot LadderFire Drill II
AIRCRAFT ENTRY
1. NORMAL/EMERGENCY ENTRY
a. OVERWING ESCAPE HATCHES, both sides, 4 places. To open, pull exterior handle, push inward at bottom and lift upward.
When doors are opened from outside, slide chutes automatically deploy. An opening door could injure rescue personnel.
b. LEFT FORWARD PASSENGER/SERVICE DOOR (Only left door has stair.) To open, using a ladder, (1) pull door handle out, (2) rotate counterclockwise, (3) push front door edge in, (4) pulling rear edge out and (5) swing door forward.
c. LEFT FORWARD PASSENGER/SERVICE DOOR (Deploying stairs.)(1) Pull door handle out and open slightly, (2) unlatch stair door byturning and holding battery switch “ON”, press and (3) hold “down”button until stair fully extends, and (4) open door fully.
d. RIGHT FORWARD EMERGENCY EXIT DOOR To open, pull handledown, located top center of door, and door lowers to open position.
NOTE: Doors are hinged at bottom edge.
e. PASSENGER AFT ENTRANCE DOOR AND STAIR Hold handle in“OPEN” position until stair is lowered. If aircraft hydraulic pressure is“OFF”, manually pull stair to maximum travel. Accumulator will provideinitial movement. (Rear ventral stairway is optional.)
2. CUT-IN
a. Cut 36” above any window with a cut out of 42” by 28” as a last resortto evacuate smoke and passengers.
WARNING
ESCAPEROPES
EXIT AND EVACUATIONSLIDE (2 PLACES)
LATCH
EXTERIORHANDLE
TOTAL FUEL CAPACITY:5,840 GALLONS(FUEL IN WINGS ONLY)
1aOVERWING EMERGENCY EIXT
EMERGENCY EXIT THROUGHSTAIRWAY OR THROUGH TAILCONE WHEN JETTISONED
FUEL TANKS (3) EVACUATION SLIDE
TAILCONEWALKWAYAND GUIDESTRAP
VENTRALSTAIRWAY
EXIT AND EVACUATION SLIDEOVERWING EMERGENCYEXITS (2 PLACES EACHSIDE)
28”
42”
36”
STAIR LIGHTSWITCH
RETURN TO OFF
CLOSED OFF OPEN
LOCKPINS
717. 717T.O
. 00-105E-9
9 AIRCRAFT EMERGENCY EGRESS1. CARGO COMPARTMENT DOOR
a. Push circular section of door handle inward to raise the handle.
b. Rotate door handle counterclockwise to unlatch door.
c. Push door upward into cargo compart-ment.
FLIGHTINTERPHONE(CREW)
SERVICEINTERPHONE(CABIN)
PUSH
PULL
(TYPICAL BOTH DOORS)
CARGO COMPARTMENTDOOR HANDLE
CARGO DOORS
DOOR/SLIDE
OXYGENBOTTLES
OVERWING EXITS
APU INTAKE(UNDERSIDE)
FLOORLEVEL
8 FEET
EXTERNAL POWER/COMM
BATTERY COMPARTMENT (UNDERSIDE)
APU AIRINTAKE
REAR STAIRCONTROL
APU EXTERNALSHUTDOWN
TAIL CONEJETTISON
DOOR/SLIDE
OVERWING EXITSDOOR/SLIDEAND STAIR
717. 717T.O
. 00-105E-9
10
AIRCRAFT FUEL AND APU SYSTEMS LOCATIONS
VENT BOX/OVERFLOW (UNDERSIDE)
FUEL TANKS FUEL LINES
VENT BOX/OVERFLOW (UNDERSIDE)
APU
APU
LOOKING FORWARD
FUEL LINES
717. 717T.O
. 00-105E-9
11
ENGINE/APU SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE/APU SHUTDOWN
a. Place fuel control levers, located on pilot’s centerconsole, to aft and OFF position.
b. Retard throttles, located on pilot’s center console, toIDLE CUTOFF position.
c. Place battery switch, located on center overhead panel,to OFF position.
NOTE: If engines fail to shutdown, pull emergency fire T-handles out, located on pilot’s center forward panel. Rotate handles as appropriate.
d. Place APU master switch, located on center overheadpanel, to OFF position.
e. On the APU ground control panel, located to left of APUaccess doors on the tail cone, place APU master switchto the APU shutoff position. Discharge fire agent 1 and/or 2 as applicable.
2. AIRCREW EXTRACTION
a. Unlatch lap belt and remove shoulder harness fromcrewmember(s).
b. If seat tracks are not damaged during crash landing,use adjustable seat controls to retract seat to aftposition. Pilot’s controls are on right side of seat whileco-pilot’s are on the left.
c. Flight crew cabin seats are equipped with lap belts andshoulder harnesses.
d. Passenger seats are only equipped with lap belts.
BATTERY QUICKDISCONNECTS (3)
LH ENGINE RH ENGINE
FIRE T - HANDLES (PULLED OUT)
717. 717T.O
. 00-105E-9
12
EMERGENCY RESCUE ACCESS
AFT LOWER CARGOCOMPARTMENT DOOR
CHOP OUT AREAS
JETTISONABLETAILCONE
OVERWING EMERGENCY EXITS
FORWARD LOWERCARGO DOOR
FORWARD PASSENGERENTRANCE DOOR
CLEARVIEW WINDOW
AVERAGE DISTANCEFLOOR LEVEL TO GROUND
AFT BULKHEAD EMERGENCY EXIT DOOR TAILCONE
ACCESS DOOR
TAILCONEJETTISON LATCH
APU COMPARTMENTACCESS DOOR
FORWARD SERVICEENTRANCE DOOR
CLEARVIEW WINDOW -CHILL PANE WITH CO2AND BREAK WITH HEAVYFIRE AXE FOR ACCESSTO HANDLE; SLIDEWINDOW AFT
WHEELS RETRACTED: 4’WHEELS EXTENDED: 8’
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE.
717. 717T.O
. 00-105E-9
CABIN CONFIGURATION12
A ATTENDANT
G GALLEY
L LAVATORY
S STOWAGE
EFFECTIVITY: 717-200 TYPE III EMERGENCY EXIT(LH & RH) 20X36” (51X91.4 CM)
TYPE III EMERGENCY EXIT(LH & RH) 20X36” (51X91.4 CM)
TYPE III EMERGENCY EXIT(LH & RH) 20X36” (51X91.4 CM)
TYPE III EMERGENCY EXIT(LH & RH) 20X36” (51X91.4 CM)
TYPE IMAIN ENTRY DOOR34X72” (86.4X183 CM)
TYPE IMAIN ENTRY DOOR34X72” (86.4X183 CM)
TYPE ISERVICE DOOR27X48” (69X122 CM)
TYPE ISERVICE DOOR27X48” (69X122 CM)
AFT ENTRY DOOR27.75X72” (70X183 CM)TAILCONE EMERGENCY EXIT
AFT ENTRY DOOR27.75X72” (70X183 CM)TAILCONE EMERGENCY EXIT
MIXED CLASS - 106 PASSENGERSFIRST CLASS - 8 SEATS ON 36” (91.4 CM) PITCH ECONOMY CLASS - 98 SEATS ON 32” (81.3 CM) PITCH
ALL ECONOMY CLASS - 117 PASSENGERS 5 - ABREAST ON 32” (91.3 CM) PITCH
L
G G
AA SGAA
L
L
AA
L
LS
G G
AA
720T.O
. 00-105E-9
720.1 AIRCRAFT PAINT SCHEME
720T.O
. 00-105E-9
720. AIRCRAFT DIMENSIONS2
The 720 was originally designated the 707-020 from amodified 707-120 design for medium-range operationfrom shorter runways. The aircraft is lighter and fasterthan the 707 and has a simplified wing design.
LENGTH 130’ 6” (39.78 M)
WING SPAN 130’ 10” (39.88 M)
720HEIGHT 41’ 5” (12.62 M)720BHEIGHT 41’ 2” (12.55 M)
720T.O
. 00-105E-9
720.3
AIRCRAFT SKIN PENETRATION POINTS
AFT CARGO DOOR CENTER CARGO DOOR FWD CARGO DOOR
8”
2”
HANDLE
PENETRATIONPOINT
PENETRATIONPOINT
PENETRATIONPOINT
HANDLE
HANDLE
10”
3”
2”
2”
FWDFWDFWD
720T.O
. 00-105E-9
720.4 AIRCRAFT SKIN PENETRATION POINTS-Continued720B TURBOFAN ENGINES
720B TURBOFAN ENGINES
LEFT SIDE OF ENGINE
RIGHT SIDE OF ENGINE
COMMON POINT (LH & RH SIDE)
RIGHT SIDE OF ENGINE
LEFT SIDE OF ENGINE
COMMON POINT (LH & RH SIDE)
FORWARDENGINE MOUNT
213.942 AFTENGINE MOUNT MID SPAR
STRUT
COWLSPLIT COWL SPLIT
ENGINE
OUTBOARD NACELLE AND STRUT LEFT SIDE VIEW
OUTBOARD NACELLE AND STRUT LEFT SIDE VIEW
ENGINE
MID SPAR
COWL SPLIT
COWLSPLIT
STRUT
213.942 AFTENGINE MOUNT
136.00 FORWARD ENGINE MOUNT
T/C FAIRING
FIRESEAL
FIRESEAL
720T.O
. 00-105E-9
720.5
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw24 Foot Ladder35 Foot LadderFire Drill IIAIRCRAFT ENTRY
1. NORMAL/EMERGENCY ENTRY
a. Overwing escape hatches both sides- Push red panel, located top center of hatches, in and push hatches inward.
b. Pull handle, located left side forward and aft entry doors, outward and rotate clockwise.
c. Pull handle, located forward and aft galley doors right side, outward and rotate counter- clockwise.
d. Press red handle, located on escape hatch top right forward crew compartment, and pull out.
2. CUT-IN
a. Cut along window lines as last resort.
NOTE: Some series are equipped with class one escape hatches.
CAUTION
For passenger and service doors, emergency slide will automatically deploy when doors are opened externally.
NOTE: Refer to the C-135 for more extensive information. Both airframes are identical except cargo and tanker capabilities.
434 GALS(1643 LITERS)
2333 GALS(8831 LITERS)
2283 GALS (8642 LITERS)
434 GALS(1643 LITERS)
2333 GALS(8831LITERS)
2283 GALS(8642 LITERS)
UTILITY & AUXILIARY RESERVOIRIN AFT CARGO COMPARTMENT
PASSENGER OXYGENSYSTEM BOTTLES IN AFTCARGO COMPARTMENT
PORTABLE OXYGENBOTTLES OR NEARFLOOR LEVEL ONPARTITIONS
HYDRAULICACCUMULATORS(RIGHT WHEELWELL AREA)
FIRE EXTINGUISHERPORTS ON ENGINERIGHT COWLING(TYPICAL EACH ENGINE)
CREW OXYGEN SYSTEMBOTTLES IN FWD LOWEREDCEILING OR FWD CARGO AREA
7306 GALS(27,656 LITERS)
ENGINE OIL TANK-EACHENGINE-RIGHT SIDEPORTABLE OXYGEN BOTTLE ON
FORWARD SIDE OF BULKHEAD
BATTERIES
28” 28”38”
1cGALLEY DOOREXTERNAL HANDLE
1aPANEL
AIRCRAFT CROSS SECTION
2aCUT-IN AREAS
NOTE: 2 inch band of contrasting color around all doors, windows and hatches operable from outside the aircraft.
GALLEY DOOR(RT SIDE ONLY)
ON CARGOACFT ONLY
AFT ENTRY DOOR
CUT-IN AREA EACH SIDE OF ACFT (NOT MARKED ON ALL ACFT)
EMERGENCY EXITS
FWD ENTRYDOOR
GALLEY DOOR(RIGHT SIDE ONLY)
1bENTRY DOOREXTERNAL HANDLE
720T.O
. 00-105E-9
720.6
ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN
a. Retard thrust levers, located on pilot’s center console, to RETARD position.
b. Place engine start levers, located on pilot’s center console, to CUT OFF position
c. Pull emergency fire T-handles, located top center above instrument panel.
d. Place engine start switches, located on pilot’s overhead panel, to OFF position.
e. In case of APU fire, pull APU fire switch, located on the upper left flight engineer’s panel, out to apply agent to APU.
f. If no APU fire, place APU master switch, located on the upper left flight engineer’s panel, to OFF position.
g. Place battery switch, located on lower right flight engineer’s panel, down to OFF position.
2. AIRCREW EXTRACTION
a. Unlatch lap belts and remove shoulder harness from crewmembers.
b. Depress seat control handles, located on flight engineer’s seat, and rotate from left to right.
NOTE: If seat tracks are not damaged during crash landing, use adjustable seat controls to retract seats to aft position.
NOTE: Passenger seats are equipped with lap belts only.
APPLICABILITY: 707-100/-200 -300/-400 720 & 720B
1cFIRE T-HANDLE
1dENGINE START SWITCHES
1gBATTERYSWITCH
1eAPU FIRE SWITCH
1fAPU MASTERSWITCH1b
START LEVERS
1aFIRE T-HANDLE
NOTE: Optional location for T-handles is on the pilot’s light shield.
720T.O
. 00-105E-9
720.7 EMERGENCY RESCUE ACCESS
CHOP OUT AREAS (NOTMARKED ON ALL AIRCRAFT)
CHOP OUT AREAS (NOTMARKED ON ALL AIRCRAFT)
AFT ENTRY DOOR
OVERWING ESCAPEHATCHES
FWD GALLEY DOOR
FWD ENTRY DOOR
FLIGHT DECK WINDOWSOPEN INTERNALLY
6 FEET 1/2 INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED
9 FEET 7INCH FLOOR LEVEL TO GROUND, WHEELS RETRACTED
AFTGALLEYDOOR
720T.O
. 00-105E-9
720. CABIN CONFIGURATION8
C CLOSET
ES ESCAPE SLIDE
G GALLEY
L LAVATORY
S DOUBLE ATTENDANT’S SEAT
EFFECTIVITY: 720, 720B (PASSENGER)
131 PASSENGERS - MIXED CLASS (DOMESTIC)
137 PASSENGERS - MIXED CLASS (INTERNATIONAL)
156* PASSENGERS - 6 A BREAST AT 34” (86.4 CM)
* ADDITIONAL PAIR OF EXITS REQUIREDFOR THIS CONFIGURATION: 149 PASSENGERSMAXIMUM ALLOWABLE WITH TWO TYPE IIIEMERGENCY EXITS.
GALLEY SERVICE DOOR 24X48” (61X121.9 CM)
TYPE III EMERGENCY EXIT(LH & RH) 20X38” (51X96.5 CM)
MAIN ENTRY DOOR34X72” (86.4X183 CM)
GALLEY SERVICE DOOR 24X48” (61X121.9 CM)
MAIN ENTRY DOOR34X72” (86.4X183 CM) 30 PASSENGERS
4 A BREAST AT 38”(96.5 CM) PITCH
101PASSENGERS6 A BREAST AT 34”(86.4 CM) PITCH
CLASS DIVIDER
18 PASSENGERS4 A BREAST AT 40”(101.6 CM) PITCH
119 PASSENGERS6 A BREAST AT 34”(86.4 CM) PITCH
TYPE III EMERGENCY EXIT(LH & RH) 20X38” (51X96.5 CM)
C L G G
S
GLLLC
LL
LG
CSS
C LG G
C L G
SLLC
G
S
L
727. 727T.O
. 00-105E-9
AIRCRAFT PAINT SCHEME1
727. 727T.O
. 00-105E-9
AIRCRAFT DIMENSIONS2
727-100/-100C 727-200
LENGTH 116’ 2” (35.41 M)
HEIGHT 31’ 9” (9.68 M)
WING SPAN 108’ (32.92 M)
LENGTH 136’ 2” (41.50 M)
HEIGHT 31’ 7” (9.61 M)
WING SPAN 108’ (32.92 M)
727. 727T.O
. 00-105E-9
3 AIRCRAFT SKIN PENETRATION POINTS
727-200 (NOT ALL -200’S)
727-200
727-100 727-200
HANDLE
HANDLE
HANDLE
HANDLE
HANDLE
PENETRATION POINTS
PENETRATION POINTSPENETRATION POINTS
PENETRATION POINTS
PENETRATION POINTS
FWD
FWD FWD FWD
FWD
18”10” 8”
10” 10”
10”10”
17”
WING TO BODYFAIRING
727. 727T.O
. 00-105E-9
4 AIRCRAFT SKIN PENETRATION POINTS-Continued
LEFT SIDE OF ENGINE
RIGHT SIDE OF ENGINE
SKIN SPLICE
COWL SPLIT
AFT COWL PANELFWD COWL PANEL
LEFT SIDE VIEWRIGHT SIDE VIEW
FWD COWLPANEL
COWLSPLIT
AFT COWLPANEL
3.75 DIAMETERCOWL VENT HOLE ATWL 209.60 AND BL 23.0 USE FOR FIREEXTINGUISHER ACCESS
COWL HINGE LINE
ENGINE
AFT MOUNT RING
NACELLE
FWD MOUNT RING
COWL SPLIT
INLET
COWL SPLIT
727-100/-200 SIDE ENGINELEFT SIDE VIEW
UP
FWD
3.75 DIAMETER COWLVENT HOLE AT NAC BL 0 USE FOR FIREEXTINGUISHER ACCESS
SKIN SPLICE727-100/-200 CENTER ENGINE
727. 727T.O
. 00-105E-9
AIRCRAFT DANGER AREAS
AXIAL DISTANCE BEHIND AIRCRAFT
DISTANCE FROMAIRCRAFT CENTERLINE
JT8D TURBOFAN ENGINE HAZARD AREASAT IDLE THRUST
INTAKE DANGER AREAS
INTAKE DANGER AREAS
18 FEET
18 FEET
4 FEET
NOSE COWLFORWARD EDGE
100 MPH(161 KMPH)
50 MPH(80 KMPH)
100 F(38 C)
200 F(93 C)
0
0
0
0
FEET
METERS
0 30 60 90 120 150
0 10 20 30 40
M30
30
20
10
0
20
10
5
0
5
10
5
F
10
727. 727T.O
. 00-105E-9
AIRCRAFT DANGER AREAS-ContinuedJT8D TURBOFAN ENGINE HAZARD AREASAT TAKEOFF THRUST
INTAKEDANGER AREAS
25 FEET
25 FEET
METERS
FEET 0 50 100 150 200 250 300
0 10 20 30 40 50 60 70 80 90 100
AXIAL DISTANCE BEHIND AIRCRAFT
DISTANCE FROMAIRCRAFT CENTERLINE
M F
30
20
10
0
10
20
10
10
5
5
0
100 F (38 C)0
150 F(65 C)
200 F(93 C)
300 F(149 C)0
0
0
0
400 MPH(644 KMPH)
300 MPH(483 KMPH)
200 MPH(322 KMPH)
150 MPH(240 KMPH)
50 MPH(80 KMPH)(TO 512 FT157M)
100 MPH(161 KMPH)
6
0
0
030
727. 727T.O
. 00-105E-9
7
AIRCRAFT COMPOSITE LOCATIONS
FIN TIP FAIRING
RAIN GUTTER
WING TO BODY FAIRING
RADOME
LEADING EDGE ACCESS PANELS
COMPOSITE LOCATIONS
727. 727T.O
. 00-105E-9
8 US MARSHALS SERVICE 727 VERSION1. US MARSHALS SERVICE 727 VERSION
Type Aircraft: 727 Saberliner used to transport prisoners.
Models involved:727-100 (93 passengers, 3 crew, and a deputy crew of 12 to 17)727-100 (95 passengers, 3 crew, and a deputy crew of 12 to 17)727-200 (configuration is similar)
Seat Positions: All seats face forward except the ones over the wingwhich face aft. A large center aisle between the seats goes from oneside to the other side where the emergency exit is over the wings.
2. PRISONER TRANSPORTATION
In 1995, the air fleets of the Marshals Service and the Immigration andNaturalization Service (INS) merged to create the Justice Prisoner andAlien Transportation System (JPATS). The merger created a moreefficient and effective system for transporting prisoners and criminalaliens. Operated by the Marshals Service, JPATS is one of the largesttransporters of prisoners in the world, handling hundreds of requestsevery day to move prisoners between judicial districts, correctionalinstitutions and foreign countries.
On average, more than 200,000 prisoner and alien movements a year arecompleted by the Marshals Service via coordinated air and groundsystems. Most of these prisoners are transported aboard Service-ownedaircraft and vehicles.
Since 1984, the Marshals Service has acquired a fleet of aircraft thatincludes three Boeing 727s, a DC-9, several smaller jets and turbopropairplanes. These planes move thousands of prisoners for the MarshalsService, Bureau of Prisons (BOP) and INS, as well as the U.S. militaryand state and local governments. Many of the airplanes were acquired atno cost through the Government Surplus Property Program and theAsset Seizure and Forfeiture Program.
The JPATS is the only government-operated, scheduled passengerairline in the nation. It serves 40 cities, and is used to move prisonersmore economically and with higher security than commercial airlines.
The U.S. Marshals Service assumes custody of individuals arrested byall federal agencies and is responsible for the housing and transportationof prisoners from the time they are brought into federal custody untilthey are either acquitted or incarcerated.
Moving thousands of prisoners and criminal aliens each year requiresextra security precautions and careful coordination. Deputy Marshals,Aviation Enforcement Officers and Aviation Safety Officers are stationedthroughout the aircraft, and prisoners wear handcuffs and leg irons in theclose confines of the aircraft cabin.
Ground security is provided by Deputy Marshals, BOP guards or INSofficers at each airport transfer point. If prisoners cannot be moved inone day, they are housed overnight at various BOP facilities. Carefulscheduling is required to ensure that each prisoner appears in court atthe designated time.
In an effort to assist state and local law enforcement agencies, theMarshals Service transports non-federal prisoners between differentjurisdictions when space is available on its aircraft.
For example, a fugitive wanted for trial in one locale may have beenapprehended in another, distant jurisdiction. However, local authoritiesare often reluctant to seek extradition of felons because of high transpor-tation and personnel costs. The Marshals Service offers state and locallaw enforcement agencies a safe and effective prisoner transportationsystem at about one-quarter of the normal cost.
727. 727T.O
. 00-105E-9
9
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw24 Foot LadderFire Drill IIAIRCRAFT ENTRY
1. NORMAL ENTRY
If Forward Entry Door is used for rescue, passenger escape chute-slide will be actuated if not disconnected from inside.
a. RIGHT FORWARD ENTRY DOOR - Pull handle outward, rotate clockwise and pull door outward to open position.
2. EMERGENCY ENTRYa. PILOT’S SLIDING WINDOW - (RH & LH) Cargo and (RH only passenger aircraft.b. OVERWING ESCAPE HATCHES - Push panel in, located top center of hatches, and push hatches inward and up.c. FORWARD ENTRY DOOR - Pull external handle, located on entry door, outward, rotate clockwise and pull door out to open position.d. MID GALLEY DOOR - Pull external handle, located on galley door right forward side, outward, rotate counterclockwise and pull door out to open position.e. AFT EXIT DOORS - Pull lower end of handle, located top center of door left side of fuselage, outward, rotate clockwise and pull door outward. (Turn handle counterclockwise on doors located on right side of fuselage.)f. AIRSTAIR ENTRY DOOR - Depress latch on access door, located right side aft fuselage, and pull handle down to release stairway. (Stairway can jack aircraft up for passenger escape in a no-gear situation.)g. AFT ENTRY DOOR - Rotate handle, located on aft entry door, clockwise and push door inward.
3. CUT-INa. Cut tenth window aft from crew compartment and fifth window forward from tail section as last resort.
NOTE: Oxygen, rafts, flashlights, and fire extinguishers are located in overhead compartments.
WARNING
NOTE: Refer to the C-22 for more extensive information. Both airframes are identical except for military configurations.
AFT CARGO FUEL TANKS (OPTIONAL) 860 US GALS (FWD) 3255 LITERS 1070 US GALS (AFT) 4050 LITERS
2FWD CARGO FUEL TANKS (OPTIONAL)810 US GALS (EACH CELL)3066 LITERS 1
1
2
VENT SURGE TANK
1793 GALS6787 LITERS
PORTABLE OXYGEN BOTTLESOXYGEN BOTTLES PASSENGERAND CREW
MAIN BATTERY
PORTABLE OXYGENBOTTLES
HYD ACCUMULATOR (WHEEL WELL)APU EMER CONTROL PANEL(LEFT WHEEL WELL AREA)
ENG OIL TANK (TYPICAL)
FIRE EXT PORT(OUTBD ENG)
HYD ACCUMULATOR(AIRSTAIR PASSAGE)
HYD RESERVOIR(AIRSTAIRPASSAGE)
PORTABLEOXYGENBOTTLEAPU
(WHEELWELL)
FUEL LINES
1793 GALS6787 LITERS
4004 GALS15,155 LITERS VENT SURGE TANK
28” 28”38” AIRCRAFTCROSS-SECTION
CUT-INAREAS
2eDOORHANDLE
1a, 2cEXTERNALHANDLE
2dMID GALLEY DOOR(RT SIDE ONLY)
2eAFT EXIT DOOR
2gAFT ENTRY DOOR
2fAFT AIRSTAIR2b
EMERGENCY OVERWINGESCAPE HATCHES
2bPANEL
HYDRAULICHANDPUMP
2fAIRSTAIR DOORRELEASE HANDLE
2dEXTERNALHANDLE
2cFWD ENTRY DOOR 3a
CUT-IN
2aPILOT’SSLIDINGWINDOW
ACCESSDOOR
727. 727T.O
. 00-105E-9
10
ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN
a. Retard thrust levers, located on pilot’s center console, to RETARD position.
b. Retard engine start levers, located on pilot’s console, to CUT OFF position.
c. In case of engine fire, pull appropriate engine fire T-handles, located on center overhead instrument panel glare shield.
NOTE: Optional location for T-handles is on the pilot’s light shield.
d. In case of APU fire, pull APU fire switch to OFF and place APU master switch to OFF, located on rear cockpit wall.
e. Lift guard and place battery switch, located on lower center flight engineer’s upper left panel, to OFF position.
2. AIRCREW EXTRACTION
a. Unlatch lap belt and remove shoulder harness from crewmembers
b. FLIGHT ENGINEER’S SEAT - Depress seat control handles and rotate seat clockwise.
c. PASSENGER’S SEATS - Passengers seats are equipped with lap belts only.
NOTE: If seat tracks are not damaged during crash landing use adjustable seat control handles to retract seats to aft position.
1cENGINE FIRE T-HANDLES 1c
ENGINE FIRE T-HANDLES
1dAPU FIRESWITCH
1dAPUMASTERSWITCH
1aTHRUSTLEVERS
1bENGINESTARTLEVERS
BULKHEAD RIGHT OFFLIGHT ENGINEER’SPANEL
727. 727T.O
. 00-105E-9
11
EMERGENCY RESCUE ACCESS
OVERWING ESCAPE HATCHES
OVERWING ESCAPE HATCHES
“CHOP OUT” AREA
CARGO DOOR (OPENS FROM INSIDE ONLY)
5 FEET 8 INCHES (FLOOR LEVEL TO GROUND, WHEELS RETRACTED)9 FEET 1 INCH (FLOOR LEVEL TO GROUND, WHEELS EXTENDED)
“CHOP OUT” AREAS
“CHOP OUT” AREA
GALLEY DOOR(MOVED FWD ON 200,REMOVED ON 200F)
FWD ENTRY DOOR
AFT ENTRY DOOR (OPENSFROM INSIDE OF THE AFTSTAIRS AREA) (AIRSTAIRMUST FIRST BE LOWERED)
AFT AIRSTAIR EXTERIORCONTROL PANEL OPERATINGINSTRUCTIONS ON ACCESSPANEL
AFT AIRSTAIR
AFT EXIT DOORS(REMOVED ON 100 AND 200F)
PILOT’S SLIDINGWINDOW
727. 727T.O
. 00-105E-9
CABIN CONFIGURATION12
EFFECTIVITY: 727-100/-100C (PASSENGER)
STOWAGE
TYPE 1 GALLEY SERVICEDOOR 33X65” (84X165 CM)
AFT ENTRY DOOR32X76 “ (81X193 CM)
WINDSCREEN
FWD ENTRY DOOR34X72 “ (97X183 CM)
TYPE IV EXIT(RH & LH) 20X38 “ (51X97 CM)TYPE III EMERGENCY
EXIT (RH & LH) 20X38 “ (51X97 CM)
106 PASSENGERS - TYPICAL MIXED CLASS (16 FIRST CLASS, 90 TOURIST)
16 PASSENGERS4 ABREAST AT 38” (97 CM) PITCH
90 PASSENGERS3 ABREAST AT 33” (84 CM) PITCH
STOWAGE34” (86 CM) TYPICAL
126 PASSENGERS - ALL TOURIST (MAXIMUM CERTIFICATED CAPACITY - 129 PASSENGERS)
C CLOSET
ES ESCAPE SLIDE
G GALLEY
L LAVATORY
S DOUBLE ATTENDANT’S SEAT
C
C
G G L
L
L
L
GG ES
ESS
LS
L
727. 727T.O
. 00-105E-9
CABIN CONFIGURATION-Continued13
ES ESCAPE SLIDE
G GALLEY
L LAVATORY
S DOUBLE ATTENDANT’S SEAT
EFFECTIVITY: 727-100C (PASSENGER/CARGO)
TYPE 1GALLEY SERVICE DOOR 33X65” (84X165 CM)
FWD ENTRY DOOR34X72 “ (97X183 CM)
SMOKEBARRIER
CARGO DOOR86X34 “ (218X340 CM) SMOKE-TIGHT PARTITION
TYPE IVTYPE III
EMERGENCY EXIT (RH & LH) 20X38 “ (51X97 CM)
AFT ENTRY DOOR32X76 “ (81X193 CM)
70 PASSENGERS
CARGO DOORCONTROL PANEL
88X108” PALLETS (122X274 CM)
88X108” PALLETS (122X274 CM)
88X108” PALLETS (122X274 CM)
56 PASSENGERS
52 PASSENGERS
G
G
S
S
S
G GL
ES
L
L
L
L
L
L
L
L
ES
ES
ES
727. 727T.O
. 00-105E-9
14
CABIN CONFIGURATION-ContinuedEFFECTIVITY: 727-100C (ALL CARGO)
CARGO DOOR86X34 “ (218X340 CM)
1 2 3 4 5 6 7 8L
L
L
L LAVATORY
CONDITIONS
HATRACKS UP
2” CLEARANCE
9 COMMERCIAL PALLETS
HIGH-PROFILE ROLLERS
PALLET VOLUME NOT INCLUDED IN CARGO VOLUME
PALLET SIZE 88X108"(223X274 CM)
88X125"(223X318 CM)
MAIN DECK
PALLET 1 359 (10.17) 401 (11.36)
PALLETS 2-8 366 (10.4) EACH2,562 (72.56)
APPROX.411 (11.6) EACH
2,877 (81.47)
LOWER DECK 890 (25.2) 890 (25.2)
TOTAL VOLUME 3,811 (107.9) 4,168 (11.8)
CARGO ENVELOPE VOLUMES IN CUBIC FEET (CUBIT METERS)
g
727. 727T.O
. 00-105E-9
15
CABIN CONFIGURATION-Continued
C CLOSET
ES ESCAPE SLIDE
G GALLEY
L LAVATORY
S DOUBLE ATTENDANT’S SEAT
EFFECTIVITY: 727-200 (PASSENGER)
L L
LS
GES
ESESG G
SES
WIND SCREEN
155 PASSENGERS - TYPICAL ALL-TOURIST(MAXIMUM CERTIFICATED CAPACITY - 189 PASSENGERS)
34” (86 CM) TYPICAL
134 PASSENGERS - TYPICAL MIXED CLASS (20 FIRST CLASS, 114 TOURIST)
AFT ENTRY DOOR32X76 “ (81X193 CM)
STOWAGE(RH & LH)
TYPE 1GALLEY SERVICE DOOR 33X65” (84X165 CM)
CLASSDIVIDER
WINDSCREEN
38” (97 CM) TYPICAL
34” (86 CM) TYPICAL
FWD ENTRY DOOR34X72 “ (97X183 CM)
TYPE III EMERGENCY EXIT (RH & LH) 20X38 “ (51X97 CM)
TYPE 1SERVICE DOOR (RH & LH)30X60” (76X152 CM)
737. 737T.O
. 00-105E-9
1 AIRCRAFT PAINT SCHEME NEXT GENERATION 737-600/-700/-800/-900
737. 737T.O
. 00-105E-9
2 AIRCRAFT DIMENSIONS
737-600
67’ 9” (20.65m)62’ 9” (19.13m)
102’ 6” (21.24m)
29’ 6” (8.84m)
15’ 10” (4.83m)
12’ 4” (3.76m)
(29.79m) 97’ 9”
41’ 3” (12.57m)
(34.32m) 112’ 7”
47’ 1” (14.35m)
(2.44 m)APPROX 8’
18’ 9” (5.72m)
SCALEMETERS 0 2 4 6
FEET 0 5 10 15 20 25
36’ 10” (11.23m)13’ 5” (4.09m)
737-700
72’ 2” (22.00m)67’ 2” (20.47m)
110’ 4” (33.63m)
34’ 0” (10.36m)
15’ 10” (4.83m)
12’ 4” (3.76m)
(32.18m) 105’ 7”
41’ 3” (12.57m)
(34.32m) 112’ 7”
47’ 1” (14.35m)
(2.44 m)APPROX 8’ 18’ 9”
(5.72m)SCALE
METERS 0 2 4 6
FEET 0 5 10 15 20 25
41’ 4” (12.60m)13’ 5” (4.09m)
NOTE: 737-600s are the current smallest version of the fleet. Earlier versions i.e., -100/-200/-300/-400/-500 models are similar until the mid 1990’s upgrades when longer versions were requested by Boeing’s customers, hence the -600/-700/-800/-900 models were developed. The earlier versions will be referred to as some of these aircraft are still in service in many countries. Military versions of the T-43 and C-40A/B/C are addressed in separate files of this manual.
(737-100/-200/-300/-400/-500 prior to engine and aircraft upgrades.)
737. 737T.O
. 00-105E-9
737-800
82’ 0” (24.99m)77’ 0” (23.47m)
129’ 6” (39.47m)
43’ 10” (13.36m)
15’ 10” (4.83m)
12’ 4” (3.76m)
(38.02m) 124’ 9”
41’ 3” (12.57m)
(34.32m) 112’ 7”
47’ 1” (14.35m)
(2.44 m)APPROX 8’
18’ 9” (5.72m)
SCALEMETERS 0 2 4 6
FEET 0 5 10 15 20 25
51’ 2” (15.60m)13’ 5” (4.09m)
737-900
87’ 2” (26.57m)82’ 2” (25.05m)
138’ 2” (41.11m)
(14.73m)
15’ 10” (4.83m)
12’ 4” (3.76m)
(40.67m) 133’ 5”
41’ 3” (12.57m)
112’ 7”
47’ 1” (14.35m)
(2.44 m)APPROX 8’ 18’ 9”
(5.72m)SCALE
METERS 0 2 4 6
FEET 0 5 10 15 20 25
56’ 4” (17.17m)13’ 5” (4.09m)
AIRCRAFT DIMENSIONS-Continued3
(34.32m)
48’ 4”
737. 737T.O
. 00-105E-9
AIRCRAFT DIMENSIONS-Continued4
737-700 WITH WINGLETS
110’ 4” (33.63m)
34’ 0” (10.36m)
15’ 10” (4.83m)
12’ 4” (3.76m)
105’ 7” (32.18m)
(12.57m)
117’ 5”(35.79m)
47’ 1” (14.35m)
(2.44m)APPROX 8’18’ 9” (5.72m)
SCALEMETERS 0 2 4 6
FEET 0 5 10 15 20 25
41’ 4” (12.60m)13’ 5” (4.09m)
75’ 6” (23.01m)
737-800 WITH WINGLETS
129’ 6” (39.47m)
43’ 10” (13.36m)
15’ 10” (4.83m)
12’ 4” (3.76m)
124’ 9” (38.02m)
41’ 2” (12.55m)
117’ 5”(35.79m) 47’ 1” (14.35m)
(2.44 m)APPROX 8’18’ 9” (5.72m)
SCALEMETERS 0 2 4 6
FEET 0 5 10 15 20 25
51’ 2” (15.60m)13’ 5” (4.09m)
85’ 4” (26.01m) 41’ 3”
737. 737T.O
. 00-105E-9
AIRCRAFT DIMENSIONS-Continued5
737-900 WITH WINGLETS
138’ 2” (42.11m)
48’ 4” (14.73m)
15’ 10” (4.83m)
12’ 4” (3.76m)
133’ 5” (40.67m)
41’ 2”
117’ 5” (35.79m)47’ 1”
(2.44 m)APPROX 8’18’ 9” (5.72m)
SCALEMETERS 0 2 4 6
FEET 0 5 10 15 20 25
56’ 4” (17.17m)13’ 5” (4.09m)
90’ 6” (27.58m)
(12.55m)
(14.35m)
737. 737T.O
. 00-105E-9
6 AIRCRAFT SKIN PENETRATION POINTS
PENETRATION POINTS
PENETRATION POINTS
FWD
HANDLE
5”
C
5”
LC
8”8”
HANDLE
FWD
L
NOTE: Typical penetration areas for all models.
737. 737T.O
. 00-105E-9
7 AIRCRAFT SKIN PENETRATION POINTS-Continued
FORWARD FAIRING
C FRONT MOUNT
C AFT MOUNT
AFT STRUT FAIRINGS THRUSTREVERSERS
SIDE COWL
3.75” DIAMETER COWL VENTHOLE AT NAC BL 0.0 USE FORFIRE EXTINGUISHER ACCESS
NOSE COWL
LL LC AFT MOUNT
C FRONT MOUNTLFORWARD FAIRING
NOSE COWLSIDE COWL
3.75” DIAMETER COWL VENTHOLE AT NAC BL 0.0 USE FORFIRE EXTINGUISHER ACCESS
INBOARDENGINE NACELLE
OUTBOARD ENGINE NACELLE
ENGINE NACELLE LEFT SIDE VIEW
ENGINE NACELLERIGHT SIDE VIEW
PENETRATIONPOINT
PENETRATION POINT PENETRATION POINT
L CNACELLE
C NACELLE L
PENETRATIONPOINT
THRUST REVERSER COWL
THRUSTREVERSERCOWL
WING WING
0.6” WIDE ANNULARVENT - USE FORFIRE EXTINGUISHERACCESS TO ENGINECORE
0.6” WIDE ANNULARVENT - USE FORFIRE EXTINGUISHERACCESS TO ENGINECORE
FAN COWL
C NACELLEL
OIL TANKFILLER DOOR
C 2.5” X 9.0” COWL VENT AT BL0USE FOR FIRE EXTINGUISHERACCESS TO FAN COMPARTMENT
L2.5” X 9.0” COWL VENT AT BL0USE FOR FIRE EXTINGUISHERACCESS TO FAN COMPARTMENT
L
FAN COWL
NACELLE CL
C
737-300/-400/-500/-600/-700/-800/-900
737-100/-200
737. 737T.O
. 00-105E-9
GRAPHITE COMPOSITESEFFECTIVITY: -100/-200/-300/-400/-500
AIRFRAME MATERIALS8
LOWER WING FIXEDLEADING EDGE PANELS
FLAPTRACKFAIRINGS
NOSELANDINGGEARDOORS
LOWER WINGFIXED TRAILINGEDGE PANELS
SPOILERS
WING TRAILING EDGEMAIN FLAP ASSEMBLY
AILERONS/TABSKINAND STRUCTURE
ENGINE COWL
RADOME
NACELLESTRUTFAIRING
UPPERWINGFIXEDLEADINGEDGEPANELS
VERTICALSTABILIZER TIP
RUDDER
HORIZONTALSTABILIZERTRAILINGEDGE
UPPER WINGFIXED TRAILINGEDGE PANELS
TAILCONE ASSEMBLY
ELEVATOR TABSTRUCTURE
MAIN LANDINGGEAR DOORSAND FAIRINGS
WING TOBODYFAIRING
737. 737T.O
. 00-105E-9
GRAPHITE OR FIBERGLASS GRAPHITE COMPOSITESEFFECTIVITY: -600/-700/-800/-900
AIRFRAME MATERIALS-Continued9
WINGLETS(AS INSTALLED)
WINGLETS(AS INSTALLED)
LOWER WING FIXEDLEADING EDGE PANELS
FLAP TRACKFAIRINGS
NOSELANDINGGEARDOORS
LOWER WINGFIXED TRAILINGEDGE PANELS
DORSALFIN SKIN
ELEVATORUPPER &LOWER SKIN
WING TRAILING EDGEMAIN FLAP ASSEMBLY
AILERONS/TAB SKINAND STRUCTURE
THRUSTREVERSER
RADOME
NACELLESTRUTFAIRING
UPPERWINGFIXEDLEADINGEDGEPANELS
VERTICALSTABILIZER TIP
TAILCONEASSEMBLY
RUDDER
VERTICALSTABILIZERTRAILINGEDGE
UPPER WINGFIXED TRAILINGEDGE PANELS
737. 737T.O
. 00-105E-9
GRAPHITE OR FIBERGLASS GRAPHITE COMPOSITESEFFECTIVITY: BOEING BUSINESS JET (BBJ)/BBJ-2
AIRFRAME MATERIALS-Continued10
WINGLETS(AS INSTALLED)
WINGLETS(AS INSTALLED)
LOWER WING FIXEDLEADING EDGE PANELS
FLAP TRACKFAIRINGS
NOSELANDINGGEARDOORS
LOWER WINGFIXED TRAILINGEDGE PANELS
DORSALFIN SKIN ELEVATOR
UPPER &LOWER SKIN
WING TRAILING EDGEMAIN FLAP ASSEMBLY
AILERONS/TAB SKINAND STRUCTURETHRUST
REVERSERRADOME
NACELLESTRUTFAIRING
UPPERWINGFIXEDLEADINGEDGEPANELS
VERTICALSTABILIZER TIP
TAILCONEASSEMBLY
RUDDER
VERTICALSTABILIZERTRAILINGEDGE
UPPER WINGFIXED TRAILINGEDGE PANELS
ELEVATOR TABSTRUCTURE
737. 737T.O
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AUXILIARY FUEL TANK CAPACITIES11
3 AFT
3 AFT/1 FWD
4 AFT 3 AFT/2 FWD 4 AFT/2 FWD 5 AFT/2 FWD
5 AFT/3 FWD
5 AFT/4 FWD
NOTE: This information includes Boeing Business Jets.
AUX FUEL GALLONS LITERS TOTAL GALLONS(ALL TANKS)
TOTALLITERS
(ALL TANKS)
3 AFT 1,485 5,685 8,360 31,710
4 AFT 2,010 7,676 8,885 33,701
3 AFT - 1 FWD 2,000 7,639 8,875 33,664
3 AFT - 2 FWD 2,530 9,647 9,405 35,672
4 AFT - 2 FWD 3,055 11,639 9,930 37,664
5 AFT - 2 FWD 3,360 12,797 10,235 38,822
5 AFT - 3 FWD 3,605 13,727 10,480 39,752
5 AFT - 4 FWD 3,850 14,656 10,725 40,681
737. 737T.O
. 00-105E-9
12
SPECIAL TOOLS/EQUIPMENTPower Rescue Saw12 Foot LadderFire Drill IIAIRCRAFT ENTRY-100/-200/-300/-400/-500 SERIES
1. NORMAL/EMERGENCY ENTRYa. Push in top center panel on overwing escape hatches, located on both fuselage sides. Push hatch inward and upward.
NOTE: Some models are equipped with stairs that can be deployed from forward and aft entry doors.
b. Pull handle on forward and aft entry doors, located left side of fuselage, outward and rotate clock- wise. Pull doors outward.
NOTE: Depress button and pull handle out, rotate clockwise to extend stairway.
c. Pull handle on right forward and aft service doors, outward and rotate counterclockwise. Pull doors outward.
CAUTION
When doors are opened from outside, chutes automatically deploy.
2. CUT-IN OR CHOP OUT AREASa. Cut along window line as the last resort.
NOTE: Refer to the T-43 for more extensive information. Both airframes are identical except for military trainer capabilities.
-100/-200
-300/-400&-500
BATTERIES
E/ECOMPARTMENT ACCESS DOOR
MAINE/E DOOR-300 (OPTIONAL
FWD ENTRY DOOR
1bFWD AND AFT ENTRYDOOR EXTERNALHANDLE (LT SIDE)
AFT ENTRYDOOR
1a EMERGENCY OVERWING EXIT HATCHES PUSH PANEL (BOTH SIDES)
ENGINE OIL TANK (ONE EACH ENGINE)RT SIDE CFM-56 LT SIDE ALL OTHERS
1cFWD AND AFT SERVICE DOOREXTERNAL HANDLE (RT SIDE)
4299GALS16,273LITERS
CREW OXYGEN BOTTLE(FWD CARGO AREA)
PASSENGEROXYGEN(OPTIONAL)
PORTABLEOXYGENBOTTLE(BEHINDCO-PILOT)
1288 GALLONS4876 LITERS
VENT SURGE TANK
VENT SURGE TANK1288 GALLONS 4876 LITERS
SYSTEM A, B & STANDBYHYD RESERVOIRS INWHEEL WELL
APU OIL TANKPORTABLE OXYGEN BOTTLES(VARIEDLOCATIONS)
APU FUEL LINESAPU EMER CONTROL PANEL (RT W W)
HYD BRAKE ACCUMULATORS (IN W W)
OPTIONAL AUX FUELTANK IN LWR AFTCARGO COMPT
390/492/984 GALLONS1476/1862/3725 LITERS
1
1
737. 737T.O
. 00-105E-9
13 EMERGENCY RESCUE ACCESS
OVERWING ESCAPE HATCHES
ADDITIONAL OVERWING ESCAPEHATCHES ( -400 ONLY)
CUT IN OR CHOP OUT AREAS
CUT-IN OR CHOP OUT AREAS LOCATED BETWEENWING FRONT SPAR AND ESCAPE HATCH (THREEBAYS) BELOW WINDOWS AND ABOVE FLOORS
AVERAGE DISTANCE -FLOOR LEVEL TO GROUNDWHEELS RETRACTED: 5 FTWHEELS EXTENDED: 8 FT. 6 IN.
FWD ENTRY DOOR
PILOT’S SLIDINGWINDOW
FWD SERVICE DOOR
CARGO DOOR (RT SIDE)OPERATING INSTRUCTIONSON DOOR
CARGO DOOR (RT SIDE)OPERATING INSTRUCTIONSON DOOR
AFT SERVICE DOOR
AFT ENTRY DOOR
EFFECTIVITY:-100/-200/-300/-400/-500 SERIES
CUT IN OR CHOP OUT AREAS
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE
CARGODOOR-200C
737. 737T.O
. 00-105E-9
14
AIRCRAFT ENTRY-ContinuedAIRCRAFT ENTRY -600/-700/-800 SERIES1. NORMAL ENTRY
NOTE: Some models are equipped with stairs that can be deployed from forward and aft entry doors.
a. Pull handle on forward and aft entry doors, located left side of fuselage, outward and rotate clockwise. Pull doors outward.
NOTE: Depress button and pull handle out, rotate clockwise to extend stairway.
b. Pull handle on right forward and aft service doors, outward and rotate counterclockwise. Pull doors outward.
c. The pilot’s sliding window can be accessed by pulling the external handle and sliding window open.
CAUTION
When doors are opened from outside, chutes automatically deploy.
BATTERY
E/E COMPARTMENTACCESS DOOR
-600/-700/-800ACCESSIBLE FROM FWDCARGO COMPARTMENT
FWD ENTRY DOOR
1aFWD AND AFT ENTRY DOOREXTERNAL HANDLE (RT SIDE)
AFT ENTRYDOOR
2aEMERGENCY OVERWING EXIT HATCHES(BOTH SIDES) (See also page 737.11)
ENGINE OIL TANK RT SIDE EACH ENGINE
1bFWD AND AFT SERVICE DOOREXTERNAL HANDLE (LT SIDE)
4299 GALS16,273 LITERS
CREW OXYGENBOTTLE (FWDCARGO AREA)
PORTABLEOXYGENBOTTLE(BEHINDCO-PILOT)
1288 GALLONS4876 LITERS
VENT SURGE TANK
1288 GALLONS 4876 LITERS
SYSTEM A, B & STANDBYHYD RESERVOIRS INWHEEL WELL
APU OIL TANK
PORTABLE OXYGEN BOTTLES(VARIEDLOCATIONS)
APU FUEL LINEAPU EMER CONTROL PANEL (RT W W)
HYD BRAKE ACCUMULATORS (IN W W)
AUXILIARYFUEL TANKLOCATIONS(BBJ ONLY)
WINGLETS (AS INSTALLED)
WINGLETS(AS INSTALLED)
1cPILOTWINDOW
737. 737T.O
. 00-105E-9
AIRCRAFT ENTRY-Continued15
2. EMERGENCY ENTRYa. Push in top center on overwing escape hatches, located on both fuselage sides (see page 737.16 for hatch locations.)
3. CARGO DOOR OPERATIONa. To open cargo door 1, unlock the external door handle.
b. Verify unlocked light in ON.
c. Hold the UP TO CANOPY switch (illustrated in red) in UP position until door motion stops.
4. CUT-IN OR CHOP OUT AREASa. Cut-in or chop out areas are located between wing front spar and escape hatch (three bays) below windows and above floors. (see page 737.11)
2aEMERGENCY OVERWINGEXIT HATCHES (BOTH SIDES)
3aEXTERNAL CARGODOOR CONTROLS
4aCUT-IN AREAS
3cUP TO CANOPY SWITCH
3bCARGO DOOR LIGHTS
737. 737T.O
. 00-105E-9
16
EMERGENCY RESCUE ACCESS
OVERWING ESCAPE HATCHES
ADDITIONAL OVERWING ESCAPEHATCHES (-800/-900 ONLY)
CUT IN OR CHOP OUT AREAS
CUT IN OR CHOP OUT AREAS LOCATEDBETWEEN WING FRONT SPAR ANDESCAPE HATCH (THREE BAYS) BELOWWINDOWS AND ABOVE FLOORS
AVERAGE DISTANCE -FLOOR LEVEL TO GROUNDWHEELS RETRACTED: 5 FTWHEELS EXTENDED: 8 FT. 6 IN.
FWD ENTRY DOOR
PILOT’SSLIDINGWINDOW
FWD SERVICE DOOR
CARGO DOOR (RT SIDE)OPERATING INSTRUCTIONSON DOOR
CARGO DOOR (RT SIDE)OPERATING INSTRUCTIONSON DOOR
AFT SERVICE DOOR
AFT ENTRY DOOR
EFFECTIVITY:-600/-700/-800 SERIES
2” WIDE BAND OF CONTRASTINGCOLOR INDICATING ALL DOORS,HATCHES AND WINDOWSEXTERNALLY OPERABLE
CARGODOOR -700C
CUT IN OR CHOP OUT AREAS
737. 737T.O
. 00-105E-9
17
ENGINE SHUTDOWN ANDAIRCREW EXTRACTION1. ENGINE SHUTDOWN (-100 thru -800 & BBJ)
a. Retard thrust levers, located on pilot’s center console, to RETARD position.
b. Retard engine start levers, located on pilot’s console, to CUT OFF position.
c. In case of engine fire, pull appropriate engine fire T-handles, located on center console forward of thrust levers. Turn right or left to discharge agent. If not illuminated, push and hold the button under the switch to release.
d. In case of APU fire, pull the APU fire T-handle, located on center console forward of thrust levers. Turn right or left to discharge agent.
e. Place APU master switch up to OFF position OR OFF position. (Switch type can vary.)
f. Lift guard and place battery switch, located on pilot’s center overhead panel, to OFF position.
2. AIRCREW EXTRACTION
a. Unlatch lap belt and remove shoulder harness from crewmembers. See page T-43.5 for view of seats and associated controls.
b. FLIGHT ENGINEER’S SEAT - Depress seat control handles and rotate seat clockwise.
c. PASSENGER’S SEATS - Passengers seats are equipped with lap belts only.
NOTE: If seat tracks are not damaged during crash landing use adjustable seat control handles to retract seats to aft position.
1eAPU MASTER SWITCH
1bENGINE START LEVERS
1dAPU FIRESWITCH
1cENGINE FIRE T-HANDLES
1fBATTERYSWITCH
1aTHRUSTLEVERS
OR
737. 737T.O
. 00-105E-9
18
CABIN CONFIGURATIONSEFFECTIVITY: -100/-200/-300/-400/-500/-600 (NO WINGLETS) (SEE SEPARATE FILES FOR T-43 AND C-40A/B/C)
MIXED CLASS8 FIRST CLASS SEATS AT 36 - IN PITCH120 ECONOMY CLASS SEATS AT 32 - PITCH
[A] ATTENDANT [C] CLOSET [G] GALLEY [L] LAVATORY [S] STORAGE
MIXED CLASS90 BUSINESS CLASS SEATS AT 34 - IN PITCH36 ECONOMY CLASS SEATS AT 32 - PITCH
SINGLE CLASS140 ECONOMY CLASS SEATS AT 32 - IN PITCH (SHOWN)OR 148 ECONOMY CLASS SEATS AT 30 - PITCH
737. 737T.O
. 00-105E-9
CABIN CONFIGURATIONS-Continued19
MIXED CLASS8 FIRST CLASS SEATS AT 36 - IN PITCH120 ECONOMY CLASS SEATS AT 32 - PITCH
[A] ATTENDANT [C] CLOSET [G] GALLEY [L] LAVATORY [S] STORAGE
MIXED CLASS90 BUSINESS CLASS SEATS AT 34 - IN PITCH36 ECONOMY CLASS SEATS AT 32 - PITCH
SINGLE CLASS140 ECONOMY CLASS SEATS AT 32 - IN PITCH (SHOWN)OR 148 ECONOMY CLASS SEATS AT 30 - PITCH
EFFECTIVITY: -700 (WITH OR WITHOUT WINGLETS)
737. 737T.O
. 00-105E-9
CABIN CONFIGURATIONS-Continued20
EFFECTIVITY: -800 (WITH OR WITHOUT WINGLETS)
MIXED CLASS8 FIRST CLASS SEATS AT 36 - IN PITCH120 ECONOMY CLASS SEATS AT 32 - PITCH
[A] ATTENDANT [C] CLOSET [G] GALLEY [L] LAVATORY [S] STORAGE
MIXED CLASS90 BUSINESS CLASS SEATS AT 34 - IN PITCH36 ECONOMY CLASS SEATS AT 32 - PITCH
SINGLE CLASS140 ECONOMY CLASS SEATS AT 32 - IN PITCH (SHOWN)OR 148 ECONOMY CLASS SEATS AT 30 - PITCH
737. 737T.O
. 00-105E-9
CABIN CONFIGURATIONS-Continued21 EFFECTIVITY: -900 (WITH OR WITHOUT WINGLETS)
MIXED CLASS12 FIRST CLASS SEATS AT 36 - IN PITCH165 ECONOMY CLASS SEATS AT 32 - PITCH
[A] ATTENDANT [C] CLOSET [G] GALLEY [L] LAVATORY
SINGLE CLASS177 ECONOMY CLASS SEATS AT 32 - IN PITCHOR 189 ECONOMY CLASS SEATS AT 31 - PITCH
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